Ôîðóì » ÀÊÒÓÀËÜÍÀß ÏÎËÈÒÈÊÀ - URGENT POLITICAL ISSUES » High Performance Navigation MEMS IMU » Îòâåòèòü
High Performance Navigation MEMS IMU
Diana: Introduction Inertial Measurement Unit, referred to as IMU, is a device to measure the attitude angle (or angular velocity) and acceleration of the three axis of the object. Gyroscope and accelerometer are the core devices of inertial navigation system (INS). With the built-in accelerometer sensor and gyroscope, the IMU can measure the linear acceleration and rotation angular velocity from three directions and can obtain the attitude, velocity and displacement information of the carrier through the resolving. ER-MIMU-02 uses MEMS accelerometer and gyroscope with high quality and reliability, RS422 and external communication, baud rate can be flexibly set between 9600~921600, through the communication protocol to set the user’s required communication baud rate. With X, Y, Z three-axis precision gyro, X, Y, Z three-axis accelerometer with high resolution, can be output by RS422 X, Y, Z three axis of gyroscope and accelerometer’s original hexadecimal complement data (including gyro hexadecimal complement the numerical temperature, angle, the accelerometer hexadecimal temperature, the acceleration hexadecimal complement number); It can also output float dimensionless values of the gyroscope and accelerometer processed by the underlying calculation. Application areas Antenna and Line of Sight Stabilization Systems Integrated Navigation Systems & Inertial Guidance System Flight Control & Guidance System Attitude Heading Reference Systems (AHRS) Stabilization of Antennas, Cameras & Platforms Aerial and Marine Geo-mapping / Surveying click here
Îòâåòîâ - 0
ïîëíàÿ âåðñèÿ ñòðàíèöû